Purkeypilot
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Last night I build my Estes Alpha III. Wood glue and epoxy cured for about 18-20 hours and this evening I flew it for the first time. The rocket was build per the instructions and was not modified in any way. An Estes A8-3 engine was used for both flights. Both launches and flights were perfect with no problems. The Ejection charge successfully deployed the recovery system (12" Estes parachute) both times and the rocket was safely recovered both times. Though each recovery system deployment was a bit non standard. Here are the details and my concerns:
Flight 1 - 4 Sheets of Estes Recovery Wadding (3-4 recommended)
The ejection charge successfully deployed the recovery system, though I noticed that the decent rate was quite a bit higher than what it should have been, and it looked like the parachute did not quite fully open, so it was logical though I was not initially sure why, as it did not look tangled from about 300' or so. It was a grass landing and there was no damage as a result of the higher than normal descent rate. Upon closer post-flight inspection, I noticed that part of the parachute had been melted by the ejection charge gasses, and one of the parachute cords/strings, had actually passed through the melted section, and then during the decent, the plastic re-solidified around the cord/string making for a weird, hang up that caused the parachute to not be able to open fully.
In the end, I choked it up to me having messed up the wadding packing (though I did gently blow on the BT and did not feel anything of significance coming out of the engine mount). I managed to work the parachute enough to be more than usable on the second flight. I also changed up slightly the way I packed the Chute/Cords, and Shock Cord (because it was the tip of the parachute that was closest to the wadding/ejection charge that got melted). This time I "Z"ed the Shock Cord and placed it into the BT, then folded the shoot and lightly wrapped the parachute cords around it.
Flight 2 - 4 Sheets of Estes Recovery Wadding
The ejection charge was again successful in deploying the recovery system, and actually the descent and landing look great! After going and recovering the rocket from about 50 yards away, while walking back to the launch pad, I began inspecting everything, and noticed about 2 of the 4 squares of recovery wadding were remaining...okay, so maybe I packed it too much? I was thinking that if it did in fact get to packed, it was more than likely the result of how I packed the Shock Cord, which then in turn packed down the wadding when I inserted the Parachute assembly. Initially, I was not too concerned about it, as I have heard many instances of wadding/dog barf, remaining in the BT after the ejection charge.
Enter getting home and giving the Alpha III a good walk around - The first think I did was remove the remaining recovery wadding. It appeared to be about 2 sheets of the the original 4. The bottom half of the wad was completely black and singed (to be expected of course). Then I noticed that the Engine Hook was a bit loose, specifically, having excess play along the longitudinal axis. So, out came the 320 lumen Surefire, and I gave a look into the Engine Mount. I noticed that there appeared to be TWO tabs when the Engine Hook mounting tongue was. It turns out that the lower one that was blacked was actually a piece of the engine mount tube wall, that had somehow gotten "peeled" down. Then I started thinking about the fact that half the ejection wadding remained in the BT, and I began thinking that it could have caused excess pressure that forced the engine down against the engine hook, which in turn forced the engine hook down and slightly tore/peeled the wall of the engine mount tube.
There is 1/4" of movement with the engine hook (along the longitudinal axis). My concerns are:
After testing with a spend A8-3 engine case, the engine can be pushed in as far as the highest engine hook position will allow and can be pulled out as far as the lowest engine hook position will allow. This is 1/4" and I'm wondering it it will effect stability at all with a CG shift. Under thrust at launch and a 7-10 G acceleration, it will be forced higher, which in theory will keep the CG above the CP. During recovery system deployment, the pressure buildup in the BT will force the engine down, lowering the GC, though at that point, it does not really matter. What I AM concerned about is if the peeling/tearing of the engine mount tube will progress and worsen after each ejection charge and recovery system deployment???
I'm going to attempt to post several pictures for everyone to see, though my attempts to post pictures a couple days ago failed (I think it may be a result of my low post count).
Any advice or insight would be greatly appreciated. Thanks in advance to all!
Flight 1 - 4 Sheets of Estes Recovery Wadding (3-4 recommended)
The ejection charge successfully deployed the recovery system, though I noticed that the decent rate was quite a bit higher than what it should have been, and it looked like the parachute did not quite fully open, so it was logical though I was not initially sure why, as it did not look tangled from about 300' or so. It was a grass landing and there was no damage as a result of the higher than normal descent rate. Upon closer post-flight inspection, I noticed that part of the parachute had been melted by the ejection charge gasses, and one of the parachute cords/strings, had actually passed through the melted section, and then during the decent, the plastic re-solidified around the cord/string making for a weird, hang up that caused the parachute to not be able to open fully.
In the end, I choked it up to me having messed up the wadding packing (though I did gently blow on the BT and did not feel anything of significance coming out of the engine mount). I managed to work the parachute enough to be more than usable on the second flight. I also changed up slightly the way I packed the Chute/Cords, and Shock Cord (because it was the tip of the parachute that was closest to the wadding/ejection charge that got melted). This time I "Z"ed the Shock Cord and placed it into the BT, then folded the shoot and lightly wrapped the parachute cords around it.
Flight 2 - 4 Sheets of Estes Recovery Wadding
The ejection charge was again successful in deploying the recovery system, and actually the descent and landing look great! After going and recovering the rocket from about 50 yards away, while walking back to the launch pad, I began inspecting everything, and noticed about 2 of the 4 squares of recovery wadding were remaining...okay, so maybe I packed it too much? I was thinking that if it did in fact get to packed, it was more than likely the result of how I packed the Shock Cord, which then in turn packed down the wadding when I inserted the Parachute assembly. Initially, I was not too concerned about it, as I have heard many instances of wadding/dog barf, remaining in the BT after the ejection charge.
Enter getting home and giving the Alpha III a good walk around - The first think I did was remove the remaining recovery wadding. It appeared to be about 2 sheets of the the original 4. The bottom half of the wad was completely black and singed (to be expected of course). Then I noticed that the Engine Hook was a bit loose, specifically, having excess play along the longitudinal axis. So, out came the 320 lumen Surefire, and I gave a look into the Engine Mount. I noticed that there appeared to be TWO tabs when the Engine Hook mounting tongue was. It turns out that the lower one that was blacked was actually a piece of the engine mount tube wall, that had somehow gotten "peeled" down. Then I started thinking about the fact that half the ejection wadding remained in the BT, and I began thinking that it could have caused excess pressure that forced the engine down against the engine hook, which in turn forced the engine hook down and slightly tore/peeled the wall of the engine mount tube.
There is 1/4" of movement with the engine hook (along the longitudinal axis). My concerns are:
After testing with a spend A8-3 engine case, the engine can be pushed in as far as the highest engine hook position will allow and can be pulled out as far as the lowest engine hook position will allow. This is 1/4" and I'm wondering it it will effect stability at all with a CG shift. Under thrust at launch and a 7-10 G acceleration, it will be forced higher, which in theory will keep the CG above the CP. During recovery system deployment, the pressure buildup in the BT will force the engine down, lowering the GC, though at that point, it does not really matter. What I AM concerned about is if the peeling/tearing of the engine mount tube will progress and worsen after each ejection charge and recovery system deployment???
I'm going to attempt to post several pictures for everyone to see, though my attempts to post pictures a couple days ago failed (I think it may be a result of my low post count).
Any advice or insight would be greatly appreciated. Thanks in advance to all!
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